[1]
F. Maggi, A. Bandera, L. Galfetti, L. T. De Luca, Th. L. Jackson, Efficient solid rocket propulsion for access to space, Acta Astronautica, 66, 11-12, (2010) 1563-1573.
DOI: 10.1016/j.actaastro.2009.10.012
Google Scholar
[2]
F. Daidzo, N. Tadahiko, K. Tekamega and S. Sedzo, Composition of the Propellant, Journal of Abstracts, no. 14 (III), 14П244П, (1978). (in Russian).
Google Scholar
[3]
V. N. Vilyunov, A. B. Vorozhtsov and Yu. V. Feshchenko, Modeling of two-phase flow of a gas mixture with burning metal particles in a semienclosed channel, Combustion, Explosion and Shock Waves, 25, 3, (1989) 296-300.
DOI: 10.1007/bf00788801
Google Scholar
[4]
F. Maggi, S. Dossi, L. T. De Luca, Combustion of metal agglomerates in a solid rocket core flow, Acta Astronautica, 92, 2, (2013) 163-171.
DOI: 10.1016/j.actaastro.2012.04.036
Google Scholar
[5]
K. N. Volkov, Qualitative analysis and numerical simulation of the movement of a particle in a channel having permeable walls with account for the action of mass forces, Journal of Engineering Physics and Thermophysics, 86, 6 (2013) 1286-1293.
DOI: 10.1007/s10891-013-0952-6
Google Scholar
[6]
A. F. Belyaev, Yu. V. Frolov, and A. I. Korotkov, Combustion and ignition of particles of finely dispersed aluminium, Combustion, Explosion and Shock Waves, 4, 3, (1968) 182-185.
DOI: 10.1007/bf00750857
Google Scholar
[7]
R. S. Larson, Prediction of Aluminum Combustion Efficiency in Solid Propellant Rocket Motors, AIAA Journal, 25, 1, (1987) 82-91.
DOI: 10.2514/3.9585
Google Scholar
[8]
S. W. Jane and A. B. Finkelstein, Laminar Pipe Flow with Injection and Suction through a Porous Wall, Transactions of ASME, 78, 4, (1956) 719-724.
DOI: 10.1115/1.4013794
Google Scholar